Method for calculating section torsional rigidity of large-opening structure of double-bubble fuselage
The invention belongs to the field of aviation structure design, and particularly relates to a double-bubble fuselage large-opening structure section torsional rigidity calculation method. Comprising the following steps: constructing a double-bubble fuselage large-opening structure analysis model; c...
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Format: | Patent |
Sprache: | chi ; eng |
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